Direct Evidence of Surface Exposed Water Ice in the Lunar Polar Regions
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The Surrender Software
Scientific image rendering for space scenes with the SurRender software Scientific image rendering for space scenes with the SurRender software R. Brochard, J. Lebreton*, C. Robin, K. Kanani, G. Jonniaux, A. Masson, N. Despré, A. Berjaoui Airbus Defence and Space, 31 rue des Cosmonautes, 31402 Toulouse Cedex, France [email protected] *Corresponding Author Abstract The autonomy of spacecrafts can advantageously be enhanced by vision-based navigation (VBN) techniques. Applications range from manoeuvers around Solar System objects and landing on planetary surfaces, to in -orbit servicing or space debris removal, and even ground imaging. The development and validation of VBN algorithms for space exploration missions relies on the availability of physically accurate relevant images. Yet archival data from past missions can rarely serve this purpose and acquiring new data is often costly. Airbus has developed the image rendering software SurRender, which addresses the specific challenges of realistic image simulation with high level of representativeness for space scenes. In this paper we introduce the software SurRender and how its unique capabilities have proved successful for a variety of applications. Images are rendered by raytracing, which implements the physical principles of geometrical light propagation. Images are rendered in physical units using a macroscopic instrument model and scene objects reflectance functions. It is specially optimized for space scenes, with huge distances between objects and scenes up to Solar System size. Raytracing conveniently tackles some important effects for VBN algorithms: image quality, eclipses, secondary illumination, subpixel limb imaging, etc. From a user standpoint, a simulation is easily setup using the available interfaces (MATLAB/Simulink, Python, and more) by specifying the position of the bodies (Sun, planets, satellites, …) over time, complex 3D shapes and material surface properties, before positioning the camera. -
A Wunda-Full World? Carbon Dioxide Ice Deposits on Umbriel and Other Uranian Moons
Icarus 290 (2017) 1–13 Contents lists available at ScienceDirect Icarus journal homepage: www.elsevier.com/locate/icarus A Wunda-full world? Carbon dioxide ice deposits on Umbriel and other Uranian moons ∗ Michael M. Sori , Jonathan Bapst, Ali M. Bramson, Shane Byrne, Margaret E. Landis Lunar and Planetary Laboratory, University of Arizona, Tucson, AZ 85721, USA a r t i c l e i n f o a b s t r a c t Article history: Carbon dioxide has been detected on the trailing hemispheres of several Uranian satellites, but the exact Received 22 June 2016 nature and distribution of the molecules remain unknown. One such satellite, Umbriel, has a prominent Revised 28 January 2017 high albedo annulus-shaped feature within the 131-km-diameter impact crater Wunda. We hypothesize Accepted 28 February 2017 that this feature is a solid deposit of CO ice. We combine thermal and ballistic transport modeling to Available online 2 March 2017 2 study the evolution of CO 2 molecules on the surface of Umbriel, a high-obliquity ( ∼98 °) body. Consid- ering processes such as sublimation and Jeans escape, we find that CO 2 ice migrates to low latitudes on geologically short (100s–1000 s of years) timescales. Crater morphology and location create a local cold trap inside Wunda, and the slopes of crater walls and a central peak explain the deposit’s annular shape. The high albedo and thermal inertia of CO 2 ice relative to regolith allows deposits 15-m-thick or greater to be stable over the age of the solar system. -
EPSC2012-280 2012 European Planetary Science Congress 2012 Eeuropeapn Planetarsy Science Ccongress C Author(S) 2012
EPSC Abstracts Vol. 7 EPSC2012-280 2012 European Planetary Science Congress 2012 EEuropeaPn PlanetarSy Science CCongress c Author(s) 2012 A Simulation of exosphere of Ceres Ruby Lin Tu (1), Wing-Huen Ip(1,2,3) and Yung-Ching Wang (3) (1) Institute of Space Science, National Central University, Taiwan, (2) Institute of Astronomy, National Central University, Taiwan, (3) Space Science Institute, Macau University Science and Technology, Macau Abstract For the purpose of tracing the ballistic trajectories of water molecules on Ceres’ surface, we have to After Vesta, the NASA Dawn spacecraft will visit the produce a surface temperature map by omitting the largest asteroid Ceres, to carry out in-depth topographic variations and the presence of impact observations of its surface morphology and craters. Our model solves the heat conduction mineralogical composition. We examine different equation by taking account of the energy balance source mechanisms of a possible surface-bounded condition at the surface boundary and the lower exosphere composed of water molecules and other boundary condition (with dT/dz=0) into account. In species. Our preliminary assessment is that solar between the heat diffusion equation is solved by wind interaction and meteoroid impact are not using the Crank-Nicolson finite difference routine adequate because of the large injection speed of the gas at production relative to the surface escape velocity of Ceres. One potential source is a low-level (1) outgassing effect from its subsurface due to thermal sublimation. In this work, the scenario of building up a tenuous exosphere by ballistic transport and the eventual recycling of the water molecules to the polar cold trap is described. -
Project Selene: AIAA Lunar Base Camp
Project Selene: AIAA Lunar Base Camp AIAA Space Mission System 2019-2020 Virginia Tech Aerospace Engineering Faculty Advisor : Dr. Kevin Shinpaugh Team Members : Olivia Arthur, Bobby Aselford, Michel Becker, Patrick Crandall, Heidi Engebreth, Maedini Jayaprakash, Logan Lark, Nico Ortiz, Matthew Pieczynski, Brendan Ventura Member AIAA Number Member AIAA Number And Signature And Signature Faculty Advisor 25807 Dr. Kevin Shinpaugh Brendan Ventura 1109196 Matthew Pieczynski 936900 Team Lead/Operations Logan Lark 902106 Heidi Engebreth 1109232 Structures & Environment Patrick Crandall 1109193 Olivia Arthur 999589 Power & Thermal Maedini Jayaprakash 1085663 Robert Aselford 1109195 CCDH/Operations Michel Becker 1109194 Nico Ortiz 1109533 Attitude, Trajectory, Orbits and Launch Vehicles Contents 1 Symbols and Acronyms 8 2 Executive Summary 9 3 Preface and Introduction 13 3.1 Project Management . 13 3.2 Problem Definition . 14 3.2.1 Background and Motivation . 14 3.2.2 RFP and Description . 14 3.2.3 Project Scope . 15 3.2.4 Disciplines . 15 3.2.5 Societal Sectors . 15 3.2.6 Assumptions . 16 3.2.7 Relevant Capital and Resources . 16 4 Value System Design 17 4.1 Introduction . 17 4.2 Analytical Hierarchical Process . 17 4.2.1 Longevity . 18 4.2.2 Expandability . 19 4.2.3 Scientific Return . 19 4.2.4 Risk . 20 4.2.5 Cost . 21 5 Initial Concept of Operations 21 5.1 Orbital Analysis . 22 5.2 Launch Vehicles . 22 6 Habitat Location 25 6.1 Introduction . 25 6.2 Region Selection . 25 6.3 Locations of Interest . 26 6.4 Eliminated Locations . 26 6.5 Remaining Locations . 27 6.6 Chosen Location . -
Green Diamond Forest Habitat Conservation Plan Appendix B
B-1 Appendix B. Profile of the Covered Species TABLE OF CONTENTS APPENDIX B. PROFILE OF THE COVERED SPECIES ................................................... B-1 B.1 NORTHERN SPOTTED OWL (STRIX OCCIDENTALIS CAURINA) .......................................... B-3 B.2 LISTING STATUS ......................................................................................................... B-3 B.2.1 Range and Distribution .......................................................................................... B-3 B.2.2 Life History ............................................................................................................ B-4 B.2.3 Habitat Requirements ............................................................................................ B-5 B.3 FISHER (PEKANIA PENNANTI) ....................................................................................... B-5 B.3.1 Listing Status ......................................................................................................... B-5 B.3.2 Range and Distribution .......................................................................................... B-6 B.3.3 Life History ............................................................................................................ B-8 B.3.4 Habitat Requirements ............................................................................................ B-9 B.3.5 Resting and Denning Habitat ............................................................................... B-10 B.3.6 Foraging Habitat ................................................................................................. -
General Index
General Index Italicized page numbers indicate figures and tables. Color plates are in- cussed; full listings of authors’ works as cited in this volume may be dicated as “pl.” Color plates 1– 40 are in part 1 and plates 41–80 are found in the bibliographical index. in part 2. Authors are listed only when their ideas or works are dis- Aa, Pieter van der (1659–1733), 1338 of military cartography, 971 934 –39; Genoa, 864 –65; Low Coun- Aa River, pl.61, 1523 of nautical charts, 1069, 1424 tries, 1257 Aachen, 1241 printing’s impact on, 607–8 of Dutch hamlets, 1264 Abate, Agostino, 857–58, 864 –65 role of sources in, 66 –67 ecclesiastical subdivisions in, 1090, 1091 Abbeys. See also Cartularies; Monasteries of Russian maps, 1873 of forests, 50 maps: property, 50–51; water system, 43 standards of, 7 German maps in context of, 1224, 1225 plans: juridical uses of, pl.61, 1523–24, studies of, 505–8, 1258 n.53 map consciousness in, 636, 661–62 1525; Wildmore Fen (in psalter), 43– 44 of surveys, 505–8, 708, 1435–36 maps in: cadastral (See Cadastral maps); Abbreviations, 1897, 1899 of town models, 489 central Italy, 909–15; characteristics of, Abreu, Lisuarte de, 1019 Acequia Imperial de Aragón, 507 874 –75, 880 –82; coloring of, 1499, Abruzzi River, 547, 570 Acerra, 951 1588; East-Central Europe, 1806, 1808; Absolutism, 831, 833, 835–36 Ackerman, James S., 427 n.2 England, 50 –51, 1595, 1599, 1603, See also Sovereigns and monarchs Aconcio, Jacopo (d. 1566), 1611 1615, 1629, 1720; France, 1497–1500, Abstraction Acosta, José de (1539–1600), 1235 1501; humanism linked to, 909–10; in- in bird’s-eye views, 688 Acquaviva, Andrea Matteo (d. -
Alternative Artemis III EVA Opportunities Near De Gerlache Crater D
Science NASADefinition-requested Team for input Artemis for the (2020 Artemis) III Science Definition Team, delivered September 8, 2020. 2044.pdf Alternative Artemis III EVA Opportunities near de Gerlache Crater D. A. Kring*, J. M. Bretzelder, I. Ganesh, N. Kumari, A. Lang, and M. A. Siegler Introduction. A topographic high point on the nearside rim of de Gerlache crater (Fig. 1) has an average solar illumination of 84% [1]. The point, site 011 of [1] and NASA’s Plan for Sustainable Lunar Exploration and Development is an attractive site to establish a solar power station if a distribution system can be developed. If that site is selected to be a long-term power station, then it may be important to avoid fouling or cluttering the location with a descent vehicle and deployed instruments until after a preliminary set of measurements has been made within the area. Thus, it may be interesting to consider other locations in the vicinity of site 011 for an Artemis III landing. Landing site and EVA options. To illustrate the types of options available, we provide a few details for an alternative area near the rim of de Gerlache crater (Fig. 1). The area occurs on an Earth-facing slope at an intersection created by the rim of de Gerlache crater and the rims of secondary craters that are mapped as the products of the Orientale basin-forming impact that occurred on the western limb of the Moon [2]. The area has a relatively smooth surface, but also contains a few small craters that may harbor small permanently shadowed regions (PSRs). -
Lunar Water ISRU Measurement Study (LWIMS): Establishing a Measurement Plan for Identifi Cation and Characterization of a Water Reserve
NASA/TM-20205008626 Lunar Water ISRU Measurement Study (LWIMS): Establishing a Measurement Plan for Identifi cation and Characterization of a Water Reserve Julie Kleinhenz Glenn Research Center, Cleveland, Ohio Amy McAdam Goddard Space Flight Center, Greenbelt, Maryland Anthony Colaprete Ames Research Center, Moff ett Field, California David Beaty Jet Propulsion Laboratory/California Institute of Technology, Pasadena, California Barbara Cohen Goddard Space Flight Center, Greenbelt, Maryland Pamela Clark Jet Propulsion Laboratory/California Institute of Technology, Pasadena, California John Gruener Johnson Space Center, Houston, Texas Jason Schuler Kennedy Space Center, Kennedy Space Center, Florida Kelsey Young Goddard Space Flight Center, Greenbelt, Maryland October 2020 NASA STI Program . in Profi le Since its founding, NASA has been dedicated • CONTRACTOR REPORT. Scientifi c and to the advancement of aeronautics and space science. technical fi ndings by NASA-sponsored The NASA Scientifi c and Technical Information (STI) contractors and grantees. Program plays a key part in helping NASA maintain this important role. • CONFERENCE PUBLICATION. Collected papers from scientifi c and technical conferences, symposia, seminars, or other The NASA STI Program operates under the auspices meetings sponsored or co-sponsored by NASA. of the Agency Chief Information Offi cer. It collects, organizes, provides for archiving, and disseminates • SPECIAL PUBLICATION. Scientifi c, NASA’s STI. The NASA STI Program provides access technical, or historical information from to the NASA Technical Report Server—Registered NASA programs, projects, and missions, often (NTRS Reg) and NASA Technical Report Server— concerned with subjects having substantial Public (NTRS) thus providing one of the largest public interest. collections of aeronautical and space science STI in the world. -
Untangling the Formation and Liberation of Water in the Lunar Regolith
Untangling the formation and liberation of water in the lunar regolith Cheng Zhua,b,1, Parker B. Crandalla,b,1, Jeffrey J. Gillis-Davisc,2, Hope A. Ishiic, John P. Bradleyc, Laura M. Corleyc, and Ralf I. Kaisera,b,2 aDepartment of Chemistry, University of Hawai‘iatManoa, Honolulu, HI 96822; bW. M. Keck Laboratory in Astrochemistry, University of Hawai‘iatManoa, Honolulu, HI 96822; and cHawai‘i Institute of Geophysics and Planetology, University of Hawai‘iatManoa, Honolulu, HI 96822 Edited by Mark H. Thiemens, University of California at San Diego, La Jolla, CA, and approved April 24, 2019 (received for review November 15, 2018) −8 −6 The source of water (H2O) and hydroxyl radicals (OH), identified between 10 and 10 torr observed either an ν(O−H) stretching − − on the lunar surface, represents a fundamental, unsolved puzzle. mode in the 2.70 μm (3,700 cm 1) to 3.33 μm (3,000 cm 1) region The interaction of solar-wind protons with silicates and oxides has exploiting infrared spectroscopy (7, 25, 26) or OH/H2Osignature been proposed as a key mechanism, but laboratory experiments using secondary-ion mass spectrometry (27) and valence electron yield conflicting results that suggest that proton implantation energy loss spectroscopy (VEEL) (28). However, contradictory alone is insufficient to generate and liberate water. Here, we dem- studies yielded no evidence of H2O/OH in proton-bombarded onstrate in laboratory simulation experiments combined with minerals in experiments performed under ultrahigh vacuum − − imaging studies that water can be efficiently generated and re- (UHV) (10 10 to 10 9 torr) (29). -
Conceptual Human-System Interface Design for a Lunar Access Vehicle
Conceptual Human-System Interface Design for a Lunar Access Vehicle Mary Cummings Enlie Wang Cristin Smith Jessica Marquez Mark Duppen Stephane Essama Massachusetts Institute of Technology* Prepared For Draper Labs Award #: SC001-018 PI: Dava Newman HAL2005-04 September, 2005 http://halab.mit.edu e-mail: [email protected] *MIT Department of Aeronautics and Astronautics, Cambridge, MA 02139 TABLE OF CONTENTS 1 INTRODUCTION..................................................................................................... 1 1.1 THE GENERAL FRAMEWORK................................................................................ 1 1.2 ORGANIZATION.................................................................................................... 2 2 H-SI BACKGROUND AND MOTIVATION ........................................................ 3 2.1 APOLLO VS. LAV H-SI........................................................................................ 3 2.2 APOLLO VS. LUNAR ACCESS REQUIREMENTS ...................................................... 4 3 THE LAV CONCEPTUAL PROTOTYPE............................................................ 5 3.1 HS-I DESIGN ASSUMPTIONS ................................................................................ 5 3.2 THE CONCEPTUAL PROTOTYPE ............................................................................ 6 3.3 LANDING ZONE (LZ) DISPLAY............................................................................. 8 3.3.1 LZ Display Introduction................................................................................. -
Planning a Mission to the Lunar South Pole
Lunar Reconnaissance Orbiter: (Diviner) Audience Planning a Mission to Grades 9-10 the Lunar South Pole Time Recommended 1-2 hours AAAS STANDARDS Learning Objectives: • 12A/H1: Exhibit traits such as curiosity, honesty, open- • Learn about recent discoveries in lunar science. ness, and skepticism when making investigations, and value those traits in others. • Deduce information from various sources of scientific data. • 12E/H4: Insist that the key assumptions and reasoning in • Use critical thinking to compare and evaluate different datasets. any argument—whether one’s own or that of others—be • Participate in team-based decision-making. made explicit; analyze the arguments for flawed assump- • Use logical arguments and supporting information to justify decisions. tions, flawed reasoning, or both; and be critical of the claims if any flaws in the argument are found. • 4A/H3: Increasingly sophisticated technology is used Preparation: to learn about the universe. Visual, radio, and X-ray See teacher procedure for any details. telescopes collect information from across the entire spectrum of electromagnetic waves; computers handle Background Information: data and complicated computations to interpret them; space probes send back data and materials from The Moon’s surface thermal environment is among the most extreme of any remote parts of the solar system; and accelerators give planetary body in the solar system. With no atmosphere to store heat or filter subatomic particles energies that simulate conditions in the Sun’s radiation, midday temperatures on the Moon’s surface can reach the stars and in the early history of the universe before 127°C (hotter than boiling water) whereas at night they can fall as low as stars formed. -
Fn000030.Pdf
1) Viaggi ed esplorazioni- 205 2) Collana Paravia Viaggi- 226 3)Collana Alpes Viaggi- 240 4) Ebraismo- 390 5) Colonialismo Fascista- 513 6) L'Illustrazione Italiana- 522 7) Storia- 546 8) Fascismo- 609 9) Spionaggio- 626 10) Letteratura italiana- 635 11) Letteratura straniera- 648 12) Il Corriere dei Piccoli-658 13) Libri per Ragazzi-693 14) Sport- 701 15) Arte-727 Le immagini di tutti i libri proposti in questo catalogo ( e molti altri) sono disponibili nella sezione RICERCA del sito www.ferraguti.it , continuamente aggiornato, che vi invitiamo a visitare. Preghiamo i gentili clienti di comunicarci l'indirizzo email, al fine di poter inviare, qualora lo gradissero, comunicazioni e cataloghi intermedi rispetto alle "classiche" pubblicazioni trimestrali. Siamo sempre interessati all'acquisto di intere biblioteche e partite o blocchi di libri, riviste e stampe d'epoca, saremo grati a chi ci fornirà opportune segnalazioni. FERRAGUTI SERVICE s.a.s. di Ferraguti Ivo & C. Borgo Bernabei 4 - 43125 Parma Tel. e Fax 0521-286980- [email protected] [email protected] P. IVA 01779470341- C.C.I.A.A. PR Reg. Ditte n. 177878 Iscrizione Tribunale di Parma n. 22291 Conto Corrente Postale n. 11724432 Catalogo numero 90- I semestre 2013- Gennaio,Febbraio, Marzo 2013 Editore: Ferraguti Service s.a.s. (Responsabile Ivo Ferraguti) Tipografie Riunite Donati - Borgo Santa Chiara 6- 43125 Parma 2 Albertini Gianni, ALLA RICERCA DEI NAUFRAGHI DELL'"ITALIA". mille kilometri sulla banchisa., Libreria d'Italia, Milano, 1929, 8o, brossura e sovracoperta., bs.,seconda ediz., pp. 165. La spedizione Nobile. Con numerose e bellissime foto. € 31,00 3 Albieri Adele, CRISTOFORO COLOMBO alla scoperta dell'America., Paravia G.B.